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Aug 31, 2024
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AEE 4263 Space Flight MechanicsCredit Hours: 3 Provides understanding of the motion of celestial objects and spacecraft under gravity. Includes analysis of the two-body and restricted three-body problems and orbital transfer using impulsive forces. Also includes designing interplanetary spacecraft trajectories for given specifications. Uses MATLAB® for numerical analyses and dynamic simulation. Prerequisite: MEE 2082 and (MTH 2201 or MTH 3200 )
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